NUMERICAL SOLUTION OF THE PROBLEM OF SUPERSONIC FLOW PAST THE LOWER SURFACE OF A DELTA WING
- 1 September 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (9) , 2224-2231
- https://doi.org/10.2514/3.2047
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Differential-geometric considerations on the hodograph transformation for irrotational conical flowArchive for Rational Mechanics and Analysis, 1960
- Exact and Approximate Solutions for the Supersonic Delta WingJournal of the Aeronautical Sciences, 1956